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Future space-transport-system compon...

Adams, Nikolaus A.

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Future space-transport-system components under high thermal and mechanical loads = results from the DFG Collaborative Research Center TRR40 /

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Future space-transport-system components under high thermal and mechanical loads/ edited by Nikolaus A. Adams ... [et al.].
其他題名:	results from the DFG Collaborative Research Center TRR40 /
其他作者:	Adams, Nikolaus A.
出版者:	Cham :Springer International Publishing : : 2021.,
面頁冊數:	ix, 419 p. :ill., digital ;24 cm.
內容註:	Collaborative Research for Future Space Transportation Systems -- Innovative Cooling for Rocket Combustion Chambers -- Film Cooling in Rocket Nozzle -- Heat Transfer in Pulsating Flow and its Impact on Temperature Distribution and Damping Performance of Acoustic Resonators -- Eﬀects of a Launcher's External Fow on a Dual-Bell Nozzle Flow -- Interaction of Wake and Propulsive Jet Flow of a Generic Space Launcher -- Numerical Analysis of the Turbulent Wake for a Generic Space Launcher with a Dual-Bell Nozzle.
Contained By:	Springer Nature eBook
標題:	Liquid propellant rockets - Fuel tanks -
電子資源:	https://doi.org/10.1007/978-3-030-53847-7
ISBN:	9783030538477

Future space-transport-system components under high thermal and mechanical loads = results from the DFG Collaborative Research Center TRR40 /
Future space-transport-system components under high thermal and mechanical loadsresults from the DFG Collaborative Research Center TRR40 /[electronic resource] :edited by Nikolaus A. Adams ... [et al.]. - Cham :Springer International Publishing :2021. - ix, 419 p. :ill., digital ;24 cm. - Notes on numerical fluid mechanics and multidisciplinary design,v.1461612-2909 ;. - Notes on numerical fluid mechanics and multidisciplinary design ;v.146..

Collaborative Research for Future Space Transportation Systems -- Innovative Cooling for Rocket Combustion Chambers -- Film Cooling in Rocket Nozzle -- Heat Transfer in Pulsating Flow and its Impact on Temperature Distribution and Damping Performance of Acoustic Resonators -- Eﬀects of a Launcher's External Fow on a Dual-Bell Nozzle Flow -- Interaction of Wake and Propulsive Jet Flow of a Generic Space Launcher -- Numerical Analysis of the Turbulent Wake for a Generic Space Launcher with a Dual-Bell Nozzle.

Open access.

This open access book presents the findings of Collaborative Research Center Transregio 40 (TRR40), initiated in July 2008 and funded by the German Research Foundation (DFG) Gathering innovative design concepts for thrust chambers and nozzles, as well as cutting-edge methods of aft-body flow control and propulsion-component cooling, it brings together fundamental research undertaken at universities, testing carried out at the German Aerospace Center (DLR) and industrial developments from the ArianeGroup. With a particular focus on heat transfer analyses and novel cooling concepts for thermally highly loaded structures, the book highlights the aft-body flow of the space transportation system and its interaction with the nozzle flow, which are especially critical during the early phase of atmospheric ascent. Moreover, it describes virtual demonstrators for combustion chambers and nozzles, and discusses their industrial applicability. As such, it is a timely resource for researchers, graduate students and practitioners.

ISBN: 9783030538477

Standard No.: 10.1007/978-3-030-53847-7doiSubjects--Topical Terms:

3486938
Liquid propellant rockets
--Fuel tanks

LC Class. No.: TL783.4 / .F87 2021

Dewey Class. No.: 629.47522

Future space-transport-system components under high thermal and mechanical loads = results from the DFG Collaborative Research Center TRR40 /
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506 $a Open access.
520 $a This open access book presents the findings of Collaborative Research Center Transregio 40 (TRR40), initiated in July 2008 and funded by the German Research Foundation (DFG) Gathering innovative design concepts for thrust chambers and nozzles, as well as cutting-edge methods of aft-body flow control and propulsion-component cooling, it brings together fundamental research undertaken at universities, testing carried out at the German Aerospace Center (DLR) and industrial developments from the ArianeGroup. With a particular focus on heat transfer analyses and novel cooling concepts for thermally highly loaded structures, the book highlights the aft-body flow of the space transportation system and its interaction with the nozzle flow, which are especially critical during the early phase of atmospheric ascent. Moreover, it describes virtual demonstrators for combustion chambers and nozzles, and discusses their industrial applicability. As such, it is a timely resource for researchers, graduate students and practitioners.
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